Q1 (a) Explain clearly how each of the following physical mechanisms causes attenuation in a silica optical fibre, stating in each case how the attenuation depends on wavelength: (i) Intrinsic absorption; (ii)Extrinsic absorption; (iii)Rayleigh scattering. [6 marks] (b) For a singlemode optical fibre explain concisely what meant by the terms mode field diameter and normalised spot size. With the aid of a simple sketch graph explain how the choice of normalised frequency V for a fibre influences the normalised spot size. [6 marks] (c) For a singlemode fibre the mode field radius w is related to the fibre core radius a by the expression: - 3/2 -6 w = 0.65 + 1.619V + 2.879V a For a given optical fibre at a wavelength of 1500 nm the mode field diameter is found to be 10.2 µm, when the normalised frequency is 2.15. Show clearly the steps involved in deciding if singlemode operation is still possible at 1320 nm for this fibre. Comment briefly on the decision with reference to the two possible definitions of cutoff wavelength in common use. [9 marks] (d) With the aid of suitable ray diagrams describe the two types of bending loss that can occur in a multimode fibre. Explain why bending loss in a singlemode fibre is wavelength dependent. [4 marks] Q2 (a) What is meant by the term “refractive index profile” for an optical fibre? Sketch each of the four refractive index profiles below and in each case state concisely a typical application were such a profile would be encountered: (i) Step index; (ii) Graded index; (iii) Depressed cladding; (iv) Triangular profile. [8 marks] (b) Describe briefly the three generic types of fibre-to-fibre joint in use in fibre systems. For each type of joint state a significant advantage and disadvantage. [6 marks] (c) Two identical multimode step index fibres are aligned together in a fibre joint. Each fibre has a radius of a µm. Assuming a uniform power distribution in the fibre core derive an expression for the coupling efficiency expressed if the only joint defect is a small lateral misalignment of d µm. [8 marks] (d) Hence determine the coupling attenuation in dB for a joint between two identical 50/125 µm fibres, assuming that the only source of attenuation is a lateral misalignment of 3 µm. [3 marks] Q1 (a) Loss mechanisms in a Silica Optical Fibre Intrinsic absorption loss: Intrinsic absorption is caused by the interaction of the light with one or more of the components of the glass itself. For silica glass there is a low loss window between 800 and 1600 nm where intrinsic absorption is negligible, by comparison with other loss mechanisms, such as scattering loss (see below). Intrinsic absorption in this window falls between 700 nm and 1500 nm, then rises again toward 1700 nm Extrinsic absorption loss: Absorption of light caused by impurities in the fibre, such as water and metals ions. One of the most common impurities is dissolved water in the glass, present as the hydroxyl or OH ion. In this case the fundamental processes takes place between 2700 nm and 4200 nm, but gives rise to so called absorption overtones at 1380, 950 and 720 nm. Extrinsic absorption depends only on the absorption wavelength of a particular impurity and on the level of the impurity. Very recently newly developed fibre manufacturing techniques have virtually eliminated absorption loss peaks giving rise to silica fibres which show no absorption peaks, This in turn opens up transmission at wavelengths circa 1400 nm and 1000 nm, which have not been utilised to date. Scattering Loss: Scattering is a process whereby all or some of the optical power in a mode is transferred into another mode. This frequently causes attenuation, since the transfer is often to a mode which does not propagate well. (also called a leaky or radiation mode). One of the most common forms of scattering is Rayleigh, a the dominant loss mechanism in the low loss silica window between 800 nm and 1600 nm. The attenuation caused by Rayleigh scattering falls off with wavelength as a function of the 4th power of wavelength. [6 marks] (b) Mode field diameter (MFD) is an important property of SM fibres. The amplitude distribution of the HE11 mode in the transverse plane in the fibre is not uniform, but is approximately gaussian in shape. The MFD is defined as the width of this amplitude distribution at a level 1/e (37%) from the peak or for power 13.5% from the peak The spot size is the mode field radius w. Its value relative to core radius “a” is given by the expression: 3 / 2 6 w = 0 . 6 5 + 1 . 6 1 9 V + 2 . 8 7 9 V a where V is the fibre “V-value”. V thus influences the spot size for given core size, as shown in the diagram below. As the V value approaches 2.4 the spot size approaches the fibre radius. For a V < 2 the spot size is significantly larger than the core size, so an optical signal is partially contained within the cladding and attenuation increases. Since beyond V = 2.4 singlemode operation is impossible for this reason V should be between about 2 and 2.4 w / a 3 2 . 5 2 1 . 5 1 1 . 2 1 . 4 1 . 6 1 . 8 2 . 0 2 . 2 2 . 4 V v a l u e N o r m a l i s e d s p o t s i z e a s a f u n c t i o n o f t h e f i b r e V v a l u e [6 marks] (c) Problem: Firstly it is noted that the two unknown parameters are the fibre core radius and the numerical aperture. Firstly calculate the actual fibre core radius “a”. Using the formula relating w/a to the normalised frequency V then since V is 2.15 then w/a is 1.19. The MFD is 10.2 µm, so the spot size is 5.1 µm. Thus the core radius is 4.28 µm. Using this value of core radius and the normalised frequency V of 2.15 it is possible to find the numerical aperture for the fibre, the only missing parameter. Now: 2 V = a . N A For a wavelength of 1500 nm from this expression the NA is found to be 0.120 Using the all of the parameter values available the fibre cutoff wavelength can be calculated by rearranging the expression above and using the cutoff value of the normalised frequency V = 2.405. 2 a N A c = V c Using the above expression the cutoff wavelength is found to be 1341 nm. Below this wavelength V > 2.405, so singlemode operation is not possible at 1320 nm according to the strict criteria above. In practice the theoretical cutoff wavelength above is difficult to measure. An alternative is EIA (Electronics Industry Association of America) cutoff wavelength, which states that the cutoff wavelength is: “The wavelength at which the power in the HE21 mode is 10% of the power in the HE11 (fundamental mode)” Since the EIA cutoff wavelength can be 100 nm less than the theoretical cutoff wavelength it is possible that singlemode operation defined as above could still take place at 1320 nm. To determine this the power in both the HE11 and the HE21 mode would need to be calculated. [9 marks] (d) Macrobending: Bending loss caused by tight cable bends. At such a bend illustrated below the conditions for total internal reflection are not maintained for some rays. This occurs because for such rays have angles of incidence to the cladding less than the critical angle in the vicinity of the bend. Thus optical power is lost into the cladding. Microbending: Bending loss caused typically by microscopic deformations of the core cladding interface. At such a deformation illustrated below the conditions for total internal reflection are not maintained and some rays and thus optical power are lost into the cladding. It is considered to be more critical than macrobending since it is largely due to processing flaws rather than mishandling. The bending loss most often associated with poor cable installation is macrobending and with poor cable design the loss is most commonly microbending. I n a s i n g l e m o d e f i b r e a s t h e s p o t s i z e o r m o d e f i e l d r a d i u s ( M F R ) i n c r e a s e s t h e l o s s a t a b e n d i n c r e a s e s , a s s h o w n i n t h e d i a g r a m b e l o w . Q u a l i t a t i v e l y t h i s i s b e c a u s e a g r e a t e r p r o p o r t i o n o f t h e m o d e f i e l d i s l o s t i f t h e M F R i s l a r g e L o w M F R = L o w e r L o s s L a r g e r M F R = H i g h e r L o s s C l a d d i n g C o r e C l a d d i n g P o w e r l o s t v i a r a d i a t i o n f r o m c l a d d i n g C o r e M o d e f i e l d M o r e p o w e r l o s t v i a r a d i a t i o n f r o m c l a d d i n g M o d e f i e l d Bending loss and wavelength in a singlemode fibre The higher the operating wavelength above the cutoff wavelength the lower the fibre V-value But a lower V-value means a larger MFR, so for longer wavelengths the MFR and thus the loss increases. Thus for example the loss due to bending can be expected to increase at 1550 nm relative to 1330 nm [4 marks] Q2 (a) The refractive index profile of a fibre is define as the relationship between refractive index and distance, in a radial fashion, from the centre of the core outwards to the cladding and beyond There are a number of common refractive index profiles (i) Step index C o r e C l a d d i n g Step index is the simplest profile, commonly found in large core multimode fibre, suited to low bandwidth, short range applications (ii) Graded index C o r e C l a d d i n g In a graded index core the refractive index follows a parabolic like form out from the centre of the core to the cladding. The result is lower modal dispersion. It is used in multimode fibre types for modest campus types distances were the limited bandwidth (typically 200-800 MHz.km) is acceptable (iii) Depressed cladding C o r e C l a d d i n g Depressed cladding profiles are a feature of some singlemode fibres, as opposed to a conventional matched cladding profile. The advantage of this profile is a reduced susceptibility to bend loss. Typically such fibre are used over longer distances, but where bend loss is an issue. (iv) Triangular profile C o r e C l a d d i n g A triangular profile is found in some singlemode fibres which are dispersion shifted. This means that the dispersion minimum no longer occurs in the 1320 nm window, but instead in the 1550 nm window. Typically used over long distances at high bit rates. [8 marks] (b) Fusion splice A fusion splice is created using a machine, which fuses the precisely aligned and cleaved fibre ends together using an electric arc. The advantages are very low loss and low material cost. A disadvantage is the high cost of the splice machine. Optical fibre connector This form of connection is analogous to an RF electrical connector. A typical connection involves two connectors and an alignment sleeve. Within each connector the fibre is epoxied in place in a precisely aligned ferrule. A connection is created by aligning the two ferrules. Connectors have the advantage that they are demountable but the disadvantages of high material cost and a higher average loss per joint. Mechanical splice A mechanical splice typically utilises a deformable precision metal tube into which the two cleaved fibres are placed. Pressure on the tube deforms the tube, holding the aligned fibre in place. Advantages include a low tooling cost and low loss and the fact that the splice is demountable. A disadvantage is the high material cost relative to a fusion splice. [6 marks] (c) Model assumes optical power is uniformly distributed over the fibre core, so it is best suited to step index multimode fibres. Diagram shows two fibre cores out of alignment by a distance "d", with the overlap of cores is shown by crosshatched area. Fibre radius is "a" Coupling efficiency is defined in this simple case as the ratio of overlap to core area d + + a In general for a circle with a radius "a" the area of a segment defined by the angle is given by: Area = 1/2 a2 ( sin ) To find the coupling efficiency we need to find the total overlap area. The overlap area is twice the area of the segment defined by the vertical line x-y in the diagram below. From the formula above we can now find the area of each segment and thus x + + a y d the overlap area To proceed we need to express the area of a segment in terms of the core radius and the misalignment "d" Consider the right angle triangle shown below as a detail of the segment. From this we can express as a function of d/a a a 22 d 2 / a + + a + / 2 d a 2 d 1 = e l g n A ) / ( s o c 2 d s n a i d a r n i s e l g n a l l A Thus: a 2 O v e r l a p a r e a = O = a ( s i n ) b u t = 1 d 2 a ( / ) 2 c o s a 1 d 1 d 2 2 a 2 a O = a ( / ) s i n ( ( / ) ) [ c o s 2 c o s ] u s e t h e i d e n t i t y s i n 2 B = 2 . s i n ( B ) . c o s ( 2 B ) a 2 1 d 2 a 1 d 2 a 1 d 2 a O = a ( / ) 2 . s i n ( ( / ) ) . c o s ( ( ( / ) ) [ c o s c o s c o s ] u s i n g t h e r i g h t a n g l e t r i a n g l e w e c a n s i m p l i f y t h u s : 2 2 a d / 2 a [ ( ) ] [ () ] 2 d / 2 a ( ) a 1 d d 2c 2 a 2 a1 O = 2 . a ( / ) / o s 2 d / 2 a ( ) 1 a 1 d d 2 2 a 2 a O = 2 . a ( / ) / c o s / O v e r l a p a r e a C o r e a r e a C o u p l i n g e f f i c i e n c y = = C o r e a r e a = . a 2 [ () ] 2 d / 2 a ( ) 1 1 d d 2 a 2 a 2 = / ( / ) / c o s [8 marks] (d) Exercise: For a 50 µm fibre the core radius “a” is 25 µm. For a misalignment “d” of 3 µm the ratio d/2a is .06. To find the attenuation at a joint we need to find the coupling efficiency, assuming that the only source of attenuation is lateral misalignment. Substituting d/2a into the coupling efficiency formula derived above we get a coupling efficiency of 92.3%. In dB this represents a loss of 0.34 dB [3 marks]